Comparison of Techniques for the Estimation of Flow Parameters of Fan Inflow Turbulence from Noisy Hot-Wire Data

被引:9
作者
Caldas, Luciano [1 ]
Kissner, Carolin [1 ]
Behn, Maximilian [1 ]
Tapken, Ulf [1 ]
Meyer, Robert [1 ]
机构
[1] German Aerosp Ctr DLR, Engine Acoust Dept, Inst Prop Technol, Mueller Breslau Str 8, D-10623 Berlin, Germany
基金
欧盟地平线“2020”;
关键词
turbulence integral length scale; hot-wire data analysis; turbulence parameter extraction; turbomachinery flow turbulence; AXIAL FANS;
D O I
10.3390/fluids6110372
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Turbulence parameters, in particular integral length scale (ILS) and turbulence intensity (Tu), are key input parameters for various applications in aerodynamics and aeroacoustics. The estimation of these parameters is typically performed using data obtained via hot-wire measurements. On the one hand, hot-wire measurements are affected by external disturbances resulting in increased measurement noise. On the other hand, commonly applied turbulence parameter estimators lack in robustness. If not addressed correctly, both issues may impede the accuracy of the turbulence parameter estimation. In this article, a procedure consisting of several signal processing steps is presented to filter non-turbulence related disturbances from the unsteady velocity data. The signal processing techniques comprise time- and frequency-domain approaches. For the turbulence parameter estimation, two different models of the turbulence spectra-the von Karman model and the Bullen model-are fitted to match the spectrum of the measured data. The results of several parameter estimation techniques are compared. Computational Fluid Dynamics (CFD) data are used to validate the estimation techniques and also to assess the influence of the variation in window size on the estimated parameters. Additionally, hot-wire data from a high-speed fan rig are analyzed. ILS and Tu are assessed at several radial positions for two fan speeds. It is found that most techniques yield similar values for ILS and Tu. The comparison of the fitted spectra with the spectra of the measured data shows a good agreement in most cases provided that a sufficiently fine frequency resolution is applied. The ratio of ILS and Tu of the velocity components in longitudinal and transverse direction allows the assessment of flow-isotropy. Results indicate that the turbulence is anisotropic for the investigated flow fields.
引用
收藏
页数:27
相关论文
共 42 条
  • [1] Airbus S.A.S., 2003, GETTING GRIPS AIRCRA
  • [2] [Anonymous], 2007, P 14 INT C SOUND VIB
  • [3] Cyclostationarity by examples
    Antoni, Jerome
    [J]. MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2009, 23 (04) : 987 - 1036
  • [4] Batchelor G. K., 1953, The Theory of Homogeneous Turbulence, DOI DOI 10.1063/1.3081561
  • [5] Behn M., 2018, P INT C FAN NOIS AER
  • [6] Statistical Error Estimation Methods for Engineering-Relevant Quantities From Scale-Resolving Simulations
    Bergmann, Michael
    Morsbach, Christian
    Ashcroft, Graham
    Kuegeler, Edmund
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2022, 144 (03):
  • [7] The effect of turbulence intensity and length scale on low-pressure turbine blade aerodynamics
    Butler, RJ
    Byerley, AR
    VanTreuren, K
    Baughn, JW
    [J]. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2001, 22 (02) : 123 - 133
  • [8] El-Gabry L.A., 2014, TM2014218403 NASA
  • [9] Envia E., 2018, Green Aviation: Reduction of Environmental Impact Through Aircraft Technology and Alternative Fuels, P3
  • [10] Fransson J.H.M., 2017, P 10 INT S TURB SHEA